Plasma processing system with locally-efficient inductive plasma coupling

ABSTRACT

An inductively coupled plasma source is provided with a peripheral ionization source for producing a high-density plasma in a vacuum chamber for semiconductor wafer coating or etching. The source includes a segmented configuration having high and low radiation segments and produces a generally ring-shaped array of energy concentrations in the plasma around the periphery of the chamber. Energy is coupled from a segmented low inductance antenna through a dielectric window or array of windows and through a segmented shield or baffle. The antenna has concentrated conductor segments through which current flows in one or more small cross-section conductors to produce high magnetic fields that couple through the high-transparency shield segments into the chamber, while alternating distributed conductor segments, formed of large cross-section conductor portions or diverging small conductor sections, permit magnetic fields to pass through or between the conductors and deliver only weak fields, which are aligned with opaque shield sections and couple insignificant energy to the plasma. The source provides spatial control of plasma energy distribution, which aids in control of the uniformity of plasma processing across the surface of the semiconductor being processed.

This is a divisional of U.S. patent application Ser. No. 10/717,268, filed Nov. 19, 2003 (, U.S. Pat. No. 7,273,533, issuing on Sep. 25, 2007).

FIELD OF INVENTION

This invention relates to high-density plasma generating devices, systems and processes, particularly for the manufacture of semiconductor wafers. In particular, the invention relates to antenna and shield structure for the production of high-density inductively coupled plasmas (ICP) for such systems and processes.

BACKGROUND OF THE INVENTION

Gas plasma generation is widely used in a variety of integrated circuit (IC) fabrication processes, including plasma etching, plasma enhanced chemical vapor deposition (PECVD), and plasma sputter deposition applications. Generally, plasmas are produced within a process chamber by introducing a process gas at vacuum pressure into the chamber and then coupling electrical energy into the chamber to create and sustain a plasma in the process gas. The plasma may exist at various ionization fractions from 10⁻⁶ up to a fully ionized plasma.

The plasma generally contains positively charged ions of working gas that are used for etching a surface of a substrate, sputtering material from a target for depositing a layer of the material onto such a substrate and ions of vaporized coating material to control the deposition of the material onto the substrate by ionized physical vapor deposition (iPVD). The plasma typically contains electrons equivalent in number to the positive charges in the plasma so that the plasma is macroscopically quasi-neutral.

Various ways of producing a plasma within a process chamber are used. Opposed electrodes can be oriented within the chamber to capacitively couple energy to the plasma. Microwave energy and electron cyclotron resonance (ECR) devices are also used. Inductive coupling of energy to the plasma is particularly desirable for producing a high-density plasma, particularly plasmas having a high-ionization fraction with a relatively low electron energy or plasma potential. Inductively coupled plasmas (ICP) often use a coil or antenna, shaped and positioned with respect to the processing chamber to inductively couple energy into the processing chamber and thus create and sustain a plasma therein.

In some ICP systems, an inductive coil or antenna is positioned around or proximate the top portion or another end of the chamber to create a plasma within the chamber. Such an antenna is positioned on one side of a dielectric plate or window in the wall of the processing chambers and electromagnetic energy from the antenna is coupled through the dielectric window and into the plasma. One suitable dielectric material for a window or chamber sidewall is quartz.

The geometry of an ICP system is a factor in determining both plasma density and uniformity, which, in turn, can affect the processing uniformity over the area of the substrate. It has often been regarded as desirable to produce a uniform, high-density plasma over a significantly large area so that large substrate sizes can be accommodated. Ultra large-scale integrated (ULSI) circuits, for example, are presently formed on wafer substrates having diameters of 200 mm and 300 mm.

In conventional sputter coating systems of the prior art, it has been recognized that the geometry of sputtering targets affected the uniformity of coatings on wafers. In U.S. Pat. No. 4,957,605, for example, it was determined that increasing material supplied from an annular ring toward the outer periphery of the target improved uniformity of coating on the wafer and improved step coverage. This patent discussed processes performed at such pressures that left line-of-sight paths for sputtered material to travel from target to wafer.

When ionized physical vapor deposition systems (iPVD) were developed, such as in U.S. Pat. No. 6,080,287, ring-shaped targets were found advantageous. An RF source in the center of the target was provided to couple energy to form a secondary plasma in the chamber that ionized material sputtered from the target. The ionized coating material aids in the coating of features on wafers as such features have become smaller. It was further found that the use of higher pressures in the chambers had advantages, as in U.S. Pat. No. 6,287,435. Such higher pressures tended to thermalize sputtered material in the chamber and masked the effects of target geometry on coating uniformity.

In etching systems and processes, pressures are usually not as high as in the high pressure iPVD systems discussed above, but because no target geometry is available, etching systems that use ICP must rely on the shape of the plasma to provide coating uniformity. In coating and etching, as well as plasma cleaning and other plasma processing systems, there remains an ongoing need for increased uniformity in the processing of wafers.

The most common inductively coupled sources have antennas in the form of coils with planar, cylindrical or dome-shaped geometry. Other coil structure includes more complex shapes having combined (hybrid) or dual coil configurations, multiple small solenoids, multiple spirals, multizone ICP enhanced PVD, torroids, transmission lines, embedded coils, planar helicon (serpentine) antennas, and parallel conductor antennas. Three-dimensional coils, and deposition baffles and Faraday shields proposed to be used with them, have been described by the present applicant in U.S. Pat. Nos. 6,237,526 and 6,474,258, and in U.S. patent application Ser. Nos. 10/080,496 and 10/338,771.

The semiconductor manufacturing tools for 300 mm wafers are becoming of increase demand, which call for larger processing chambers, typically more than 450 mm in diameter. Such chamber enlargement is needed to reduce plasma losses within the processing zone by reducing the effect of the chamber walls on the bulk plasma, and to accommodate inside the chamber hardware such as shields, lamps, diagnostic devices, monitoring and control instrumentation, that are becoming increasingly required. For such chambers, the inductive elements are made larger as well, in a range of from 400 to 500 mm diameter for cylindrical or solenoid coils and up to 350 mm for spiral antennas used to inductively couple energy into the chambers for the processing of 300 mm wafer.

Increased coil size has required larger dielectric windows to allow RF energy to penetrate into plasma efficiently and to withstand atmospheric forces. Scaling up an external antenna for large area plasma in a conventional inductively coupled discharge meets such difficulties as requiring a thick dielectric window, a large inductance of antenna, and an enormous increase in power required to provide identical plasma conditions for etching or deposition. For example, inductance of the antenna is proportional to the square of the number of turns, and voltage drop across the antenna increases with number of turns. The voltage at the ends of such large scaled antennas can easily reach values above 10 kV at typical coil currents at the industrial frequency of 13.56 MHz. Such a high voltage is a hazard and results in an intense capacitive coupling between the antenna and the plasma, and an increased potential for sparking and arcing.

Etch uniformity at the wafer is given by ion flux towards the wafer and it is determined by plasma density distribution. Typically, an ICP source with a spiral coil produces a plasma distribution with a peak at its center. Use of solenoids with larger diameters is limited due to induced high voltages at such coils. The geometry of an inductively coupled plasma source, specifically of the antenna, is a significant factor in determining both the plasma and processing uniformity over a large area. With ICP sources, plasma is excited by heating electrons in the plasma region near the vacuum side of the dielectric window by oscillating inductive fields produced by the antenna and coupled through the dielectric window. Inductive currents, which heat the plasma electrons, are derived from RF magnetic fields produced by RF currents in antenna. The spatial distribution of the magnetic field is a function of the sum of the fields produced by each portion of the antenna conductor. The geometry of the inductive antenna can in large part determine spatial distribution of the plasma ion density within the reactor chamber.

In some cases, a shield that is transparent to the inductive component of the electromagnetic field is used to suppress the capacitive coupling from antenna to plasma and to prevent a conductive or contaminating layer from building up on the dielectric window. The geometry and structure of such a shield can have an effect on the spatial distribution of plasma inside the chamber as well.

SUMMARY OF THE INVENTION

An objective of the present invention is to improve the plasma processing uniformity on semiconductor wafers, particularly in applications involving etching or higher pressure coating processes.

A more particular objective of the present invention is to provide a plasma source for utilization in the plasma processing of large area substrates, including by processes of plasma etching, plasma deposition and plasma cleaning.

Another objective of the invention is to provide a low inductance inductive device.

An additional objective of the invention is to provide a highly effective and simplified plasma source and reduced chamber cost. A more particular objective of the invention is to provide a reduced cost of ownership of ICP plasma processing equipment, and particularly to provide an ICP source that is economically and relatively easily manufactured and maintained.

In accordance with the principles of the present invention, an active peripheral ionization source is provided for use in producing a plasma density that yields uniform plasma processing for semiconductor wafers, particularly for large wafers such as 300 mm wafers. Further in accordance with the present invention, an ICP source is provided with a low inductance inductive radiating device in the form of an antenna or coil for coupling energy into the vacuum plasma processing chamber.

In various embodiments of the invention, an ICP source is provided with a segmented antenna having locally differing parameters and providing a generally lowered impedance. The antenna is configured to produce enhanced peripheral ionization. Typically, such ionization produces a generally ring-shaped plasma which compensates for the overall chamber and source geometry so as to produce a uniform effective plasma at the surface of the wafer for processing the wafer. The ring-shaped plasma is, in many embodiments, in the form of an annular array of alternating high and low power concentration regions around the periphery of the chamber.

In accordance with various embodiments of the invention, deposition and etching machines for semiconductor wafer processing are provided with an ICP source having multiple sections, providing dual performance. Certain portions of the source are provided with shield sections having high-transparency to the RF magnetic field from adjacent sections of an antenna that are configured to deliver maximum power into the plasma. These portions of the source are arranged in a ring in a peripheral area of the chamber and operate in the most effective mode of energy conversion for coupling power into the plasma. Other portions of the source are provided with shield sections that are opaque to the RF magnetic field from adjacent sections of the antenna that are configured to operate at low efficiency to reduce the amount of power delivered to adjacent hardware. In these portions of the source, the antenna is shielded from the plasma by the opaque shield sections, which also provide complete shielding of the dielectric wall against contamination from the plasma.

In its preferred embodiments, such a device is provided with a single inductive element instead of spatially distributed multiple inductive coils.

In certain embodiments of the invention, dielectric window size and thickness are reduced to increase ICP efficiency. ICP efficiency may also be reduced in locations where it is not required to deposit high RF power into plasma.

In particular embodiments of the invention, an antenna is provided with sections that differ in current carrying cross-section. The provision of such a cross-section that differs from one section to another concentrates the antenna current in one section and spreads it in another, thereby producing respectively higher and lower radiation or antenna efficiency from one such section to the other.

In certain embodiments, a spiral or annular 3-D antenna has a conductor element that defines angular portions, in some of which the conductors are spatially concentrated while in others the conductors are spatially distributed, producing respectively higher and lower radiation or coupling efficiency of RF energy from such portions. In many embodiments, closely-grouped tubular conductor segments form the spatially concentrated segments while spread-out or divergent conductor segments, or large surface-area segments, form the spatially distributed segments.

In some embodiments, an antenna is provided with a continuous conductor having differing cross-section segments that define different angular portions around the center of the chamber. In some such portions, the conductor has a large physical cross-section that presents an extended current-carrying surface from which weaker magnetic flux radiates than in portions having small physical cross-sections, which present a smaller current-carrying surface from which the radiation of magnetic flux is stronger.

The embodiments having the varying cross-section conductors and those having the single cross-section conductor present highly concentrated currents in the high-efficiency sections and spatially distributed currents in the low-efficiency sections.

A deposition baffle or shield may be provided with the antenna that is electromagnetically opaque in portions that coincide with the low-efficiency portions of the antenna, or segmented windows may be provided in the chamber wall that so coincide.

Serial connection of multiple conductor sectors can be arranged in different patterns, so common high magnetic flux channels are created by multiple sectors with small conductive cross-section, and low flux channels, are created by sectors with large conductive cross-section. To excite and sustain plasma effectively, small conductive cross-section sectors may be positioned next to the dielectric window that separates the vacuum from atmosphere.

Localization of the inductive coupling brings valuable benefits in plasma source design and its performance. Sector efficiently coupled to the plasma by inductive coupling from small conductive cross-section sectors can be by design positioned in a place required to produce plasma processing uniformity, localized plasma sustaining or ignition, power distribution, etc. Effective RF power delivery into some areas may be provided while power delivery may be reduced or eliminated in other areas. Due to localized inductive coupling efficiency, the RF transparent dielectric window need not extend over the full face of the inductive element, but only over areas where effective coupling need occur. Smaller dielectric windows can be used, which may be much thinner since they need to withstand significantly smaller atmospheric forces than in the case of single large-scale windows. Even large dielectric windows can be made of thinner material because they can be supported by rigid structure of the shields where very low inductive coupling between inductive element and plasma occurs. The total inductance of a segmented antenna will be lower than with a non-segmented coil. Inductance can be adjusted to a particular value by choosing appropriate ratios and geometries for the different sectors.

Advantages of certain embodiments of the invention are that existing RF source hardware of many existing plasma processing systems can be reduced in size and power levels, or even reduced to single antenna which is integrated with substrate holder plasma source, that will be sufficient to provide plasma to process wafers placed on the holder. Efficiency can be provided by thus generating plasma in the vicinity of the wafer where it affects immediately the plasma distribution above the wafer and not require oversized RF power supplies.

Embodiments of the present invention provide advantages that include greatly increasing, for example doubling, the lifetime of the dielectric wall or window of the chamber, which may be rotated or otherwise shifted to move the localized areas of deposition across the wall or window. Only certain portions of a bell jar, for example, would be directly exposed to plasma and contamination where a shield is segmented into sections of differing opacity.

Deposition shields provided with the invention typically have reduced ohmic losses. Antennas provide reliable plasma ignition. The antennas allow the use of partially opaque deposition shields without loss of power due to reduced inductive coupling. Increased RF power coupling into plasma occurs in pre-selected locations, which can be provided and tailored by inductive element design, such as by optimizing the pitch or ratio between low and high-transmission areas of the deposition shield. Intense RF magnetic fields are generated locally, increasing power coupling into plasma, through short slots in a deposition shield.

These and other objectives and advantages of the present invention will be more readily apparent from the following detailed description.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a simplified diagram of a prior art ionized physical vapor deposition apparatus of one type to which certain embodiments of the present invention can be applied.

FIG. 1A is a simplified diagram of a prior art plasma etch or plasma cleaning apparatus of one type to which other embodiments of the present invention can be applied.

FIG. 2 is an expanded perspective view of a peripheral ionization ICP source according to certain embodiments of the present invention.

FIG. 2A is a top diagrammatic view of a prior art ICP source for an iPVD apparatus of the type illustrated in FIG. 1.

FIG. 2B is a three-dimensional graph of plasma power distribution produced by the source of FIG. 2A.

FIG. 2C is a top diagrammatic view of an ICP source for an iPVD apparatus of the type illustrated in FIG. 1 according to one embodiment of the present invention.

FIG. 2D is a three-dimensional graph of plasma power distribution produced by the source of FIG. 2C.

FIG. 2E is a top diagrammatic view of an ICP source for an iPVD apparatus of the type illustrated in FIG. 1 according to another embodiment of the present invention.

FIG. 2F is a three-dimensional graph of plasma power distribution produced by the source of FIG. 2E.

FIG. 3 is a perspective diagram of a section of an antenna conductor for the ICP source of FIG. 2E.

FIGS. 3A-3E are perspective diagrams of alternative embodiments of the conductor of FIG. 3.

FIG. 4 is a cut-away perspective view of a cathode assembly for an iPVD apparatus having an ICP source according to one embodiment or the present invention.

FIGS. 4A-4F are perspective diagrams of alternative embodiments of the ICP source of FIG. 4.

FIG. 5 is a diagrammatic perspective view of an ICP source for an etch apparatus according to an embodiment of the present invention.

FIGS. 5A-5B are alternative antennas for the source of FIG. 5.

FIG. 6 is a diagrammatic perspective view of an ICP source for an etch apparatus similar to FIG. 5 according to another embodiment of the present invention.

FIG. 6A is an alternative antenna for the source of FIGS. 5 and 6.

FIG. 6B is a deposition baffle for the antenna of FIG. 6A.

FIG. 6C is a power distribution diagram for an ICP source having the antenna of FIG. 6A and baffle of FIG. 6B.

FIG. 6D is an alternative antenna for the source of FIGS. 5 and 6.

FIG. 6E is a deposition baffle for the antenna of FIG. 6D.

FIG. 6F is a power distribution diagram for an ICP source having the antenna of FIG. 6D and baffle of FIG. 6E.

FIG. 6G is an alternative antenna for the source of FIGS. 5 and 6.

FIG. 6H is a deposition baffle for the antenna of FIG. 6G.

FIG. 6J is a power distribution diagram for an ICP source having the antenna of FIG. 6G and baffle of FIG. 6H.

FIGS. 7A-7C are perspective diagrams of alternative ICP sources for the iPVD apparatus cathode assembly of FIG. 4.

DETAILED DESCRIPTION

The ICP source of the present invention can be used in various plasma processing systems, such as those for performing sputter etching and deposition processes, plasma-enhanced CVD (PECVD) processes, ionized PVD (iPVD) processes, and reactive ion etching processes (RIE). FIG. 1 illustrates an iPVD apparatus 10 of a type for the manufacture of semiconductor wafers in which embodiments of the invention are described below. Examples of semiconductor wafer processing machines of the iPVD type are described in U.S. Pat. Nos. 6,080,287 and 6,287,435, both hereby expressly incorporated by reference herein.

The iPVD apparatus 10 includes a vacuum processing chamber 12 enclosed in a chamber wall 11 having an opening 13 at the top thereof in which is mounted an ionized sputtering material source 20, which seals the opening 13 to isolate the vacuum within the chamber 12 from external ambient atmosphere. Within the chamber 12 is a wafer support 14 that holds a semiconductor wafer 15 with a side thereof to be processed facing the opening 13. The ionized material source 20 includes a magnetron cathode assembly 21 that includes an annular target 22, which is the source of the coating material, typically but not necessarily a metal. The cathode assembly also includes a power supply (not shown) for applying a negative DC sputtering potential to the target 22 and a permanent magnet assembly 23 situated behind the target 22, which traps electrons energized by the DC potential over the surface of the target 22 to form a primary plasma that produces ions in the gas within the chamber to sputter material from the target 22.

In the source 20, the target 22 is annular and surrounds a dielectric window 25, typically formed of quartz or alumina, that is sealed to the target 22 at its center. The target 22 and the window 25 form part of a vacuum enclosure for the chamber 12 along with the chamber wall 11. An RF ICP source 24 is situated at the window 25 and couples RF energy into the chamber 12 to energize a secondary high-density inductively coupled plasma within the chamber 12. The RF ICP source 24 includes an antenna or coil 26 situated on the atmospheric side of the window 25 and a deposition baffle or shield 27 that covers the window 25 on the inside of the chamber 12. An RF generator (not shown) is connected across the leads of the antenna 26 through a suitable matching network. Typically, the RF generator operates at the industrial frequency of 13.56 MHz. Pressures in the chamber 12 for iPVD usually fall in the range from 10 mTorr to 150 mTorr.

The antenna 26 and the shield 27 are designed together to most effectively inductively couple RF energy from the antenna 26 into the chamber 12 through the window 25 and shield 27, with low capacitive coupling from the antenna 26 into the chamber 12 that would impose a voltage on the plasma. The shield 27 is further configured to protect the window 25 from accumulated deposition, which, where the coating material is metal in particular, renders the window 25 opaque to radiation from the antenna, and interferes with the coupling of energy into the plasma. Details of antennas and the accompanying shields are described in U.S. Pat. Nos. 6,237,526 and 6,474,258, and U.S. patent application Ser. Nos. 10/080,496 and 10/338,771, all hereby expressly incorporated by reference herein.

FIG. 1A illustrates an etch module, in particular an ICP sputter-clean process module 30, to which principles of the present invention can be applied. The module 30 has a vacuum processing chamber 32 enclosed therein by a chamber wall 31, illustrated as a quartz bell jar. Etch modules having metal-walled chambers with limited dielectric windows therein are also used for etch purposes and may also benefit from principles of the invention, as, for example, described in U.S. patent application Ser. No. 09/875,339, hereby expressly incorporated by reference herein. In the chamber 32, wafer 15 to be processed is supported on an RF biased substrate holder 33, to which it maybe held by mechanical clamps, electrostatic chucks or other clamping structure (not shown). RF power is typically biased capacitively to the substrate holder 33 from an RF generator 34 through a matching network 35, and typically also through a capacitor 36.

When RF power is applied, a plasma is generated in the vacuum chamber 32, which typically is filled with an inert gas such as Argon, usually at pressures of from 0.1 to 10 mTorr. The substrate support 33 is generally biased negatively so that positive ions are accelerated towards the substrate 15 with energy sufficient to sputter etch materials from the surface of the wafer 15. Sputter etch rate depends on the energy and ion flux density. Energy is determined by the potential difference between plasma and substrate 15 on the substrate holder 33. Ion flux is determined by bulk plasma density. To increase ion flux towards the surface of the substrate 15, RF energy may be coupled into the chamber 32 by an antenna or coil 38 to form a high-density ICP in the chamber 32.

High-density inductively coupled plasmas have produced processing effects that are greater at the center of the wafers 15 than toward the wafer edges. Applicant has proposed to improve uniformity with a ring-shaped plasma in U.S. Pat. No. 6,534,493, hereby expressly incorporated by reference herein. In that patent, the use of a permanent magnet to shape the plasma was proposed. With the present invention, shaping of a plasma is provided by use of a locally-efficient RF ICP source. Such a source uses, for example, a series or arrangement of locally-efficient plasma generation, for example, by generating concentrations of plasma energy in a ring within the vacuum processing chamber. In the described embodiments, this local coupling efficiency is achieved by various embodiments of locally-efficient antenna structure, locally transparent shield structure, and combinations of antenna and shield structure. The shaped plasma is achieved in certain of the described embodiments by providing such locally-efficient structure in a peripheral ionization source in semiconductor wafer etching and coating processes and systems.

FIG. 2 illustrates an embodiment of a peripheral ionization source 39 embodying principles of the present invention. The peripheral ionization source 39 includes a segmented antenna 40 and preferably also a deposition baffle or shield 50, which may be installed in an ICP processing machine, aligned with each other on opposite sides of a dielectric section of, or window 25 in, the vacuum chamber wall of the apparatus. The antenna 40 is located in an atmospheric pressure environment outside of the window 25 while the baffle 50 is located in the vacuum chamber inside of the window 25. The antenna 40 is formed of one or more windings of a conductor 43 having high-efficiency, relatively high-inductance sections 41 alternating with low-efficiency, relatively low-inductance sections 42. The baffle 50, when employed, is formed of relatively transparent areas 51 alternating with relatively opaque areas 52. Installed in the processing apparatus, the high-efficiency sections 41 of the antenna 40 align with the high-transparency sections 51 of the baffle 50 while the low-efficiency sections 42 of the antenna 40 align with the low-transparency sections 52 of the baffle 50.

FIG. 2A is a top view of one embodiment of a three-dimensional coil 26 a of a type described in U.S. Pat. No. 6,474,258 for use in an iPVD apparatus of the type described in U.S. Pat. No. 6,287,435 and depicted by the diagram of FIG. 1. Also illustrated is one embodiment of a deposition baffle 27 a, also as described in those patents. The intervening window 25 is omitted. FIG. 2B is a graph illustrating power density 29 deposited from the antenna 26 a into the chamber 12 immediately below the deposition baffle 27 a. The power density tends to be greater toward the centerline of the chamber 12 and wafer 15. This is one representation of the prior art.

According to one aspect of the present invention, a segmented peripheral ionization source 39 a is formed by providing a segmented deposition baffle 50 a in combination with a spiral coil 26 b, as illustrated in FIG. 2C. The baffle 50 a has six relatively RF-transparent sections 51 a alternating with six relatively RF-opaque sections 52 a distributed in a circle around the centerline of the chamber and of the coil 26 b. As a result, a plasma density distribution 60 a is provided with six localized regions 61 a of high-density plasma formation opposite the transparent sections 51 a from the coil 26 b, where the coupling is locally-efficient, as illustrated in the graph of FIG. 2D. Regions 62 a between the six regions 61 a are adjacent the opaque sections 52 a where coupling through the baffle 50 a is inefficient.

According to another aspect of the invention, a segmented antenna 40 a is provided, which is illustrated in FIG. 2E in combination with the segmented baffle 50 a, forming a peripheral ionization source 39 b similar to the embodiment illustrated in FIG. 2. The segmented antenna 40 a provides an advantageously reduced impedance when compared to the embodiment 39 a having the coil 26 b. The antenna 40 a has six relatively high-inductance sections 41 a, from which field production is relatively efficient, alternating with six relatively low-inductance sections 42 a, from which field production is inefficient, distributed in a circle around the centerline of the chamber 12. The segmented antenna 40 a may be used in combination with a baffle, for example the baffle 50 a, with the transparent sections 51 a thereof aligning with the relatively high-inductance sections 41 a of the antenna 40 a and the opaque sections 52 a of the baffle 50 a aligning with the relatively low-inductance sections 42 a of the antenna 40 a. As a result, a plasma density distribution 60 b is provided with six localized regions 61 b of high-density plasma formation opposite the transparent sections 51 a from the antenna sections 41 a, where the field production and coupling are locally-efficient, as illustrated in the graph of FIG. 2F. Regions 62 b between the six regions 61 b are opposite the opaque sections 52 a from the antenna sections 42 a where field production by the antenna 40 a and the coupling through the baffle 50 a are inefficient.

In accordance with the preferred embodiment of the present invention as best shown in FIG. 4, high-density inductively coupled plasmas (ICP) for semiconductor coating and etching systems and processes is generated and maintained by a shaped peripheral inductive element that allows spatial distribution of the RF power into the plasma at locally enhanced ICP efficiency. The peripheral inductive element includes either or both of an antenna 40 and shield structure 50. For purposes of discussion, the antenna 40 refers to any of the various embodiments, illustrated or otherwise, such as antenna 40 a (FIG. 2E), and the shield structure 50 refers to any of the various embodiments, illustrated or otherwise, such as baffle 50 a (FIG. 2C). Similar references are made to sections 41, 42, 51 and 52 of this structure and to plasma distribution 60 a, 60 b and the features 61 a, 61 b and 62 a, 62 b thereof.

A feature of the segmented antenna element 50 is that its total inductance is lower than for a non-segmented antenna, such as antenna 26 a or 26 b, thereby making it technically more suitable for large area plasma processing systems, such as for 300 mm wafers 15, while maintaining the simplicity typical of smaller size ICP sources. The segmented antenna 40 is provided with an azimuthally modulated pitch that provides a spatial distribution of the rf power deposited into plasma, reduced ohmic losses in the deposition shield 50, low-inductance, and locally enhanced RF power density distribution 60 a, 60 b into plasma. The spatial RF power density distribution 60 a, 60 b allows for the design of a deposition shield 50 with enhanced shielding performance.

Design of the conductors of the segmented antenna or antennas 40 may be understood by reference to FIG. 3. An antenna 40 may be formed of a serial conductor 43, through which may be considered as instantaneously flowing in a direction indicated by arrows 44, that consists of the serial connection of two sizes of conductors or conductor sectors 45 and 46, each with respectively different cross-sections S₁ and S₂ in a direction perpendicular to the current flow 44. Each of the different cross-section conductor sectors 45 and 46 has a length defined as L₁ and L₂, respectively, in a direction parallel to the current flow 44. Accordingly, the conductor 43 may be described as having a “filling factor”, Φ, which is defined as a ratio of a conductor length L₂, related to a large cross-section portion 46 to a total conductor length L₁ and L₂, (sum of conductor lengths both for small and large cross-section portions 45 and 46), e.g. Φ=L₂/(L₁+L₂). The conductor may also be defined in part by the “cross-section ratio”, Θ, as the ratio of the cross-sectional area S₂ of the large cross-section segment 46 to the area S₁ of the small cross-section segment 45, or Θ=S₂/S₁.

A constant RF current flows through the conductor 43. At the RF frequencies used, this current flows close to the surface of the conductor 43 in the manner that it would flow through a cage of wires surrounding a space of the solid conductor's cross-section. In the case of the smaller cross-section segment 45, the surface current density is significantly higher than in the case of the larger cross-section segment 46. Consequently, the induced RF magnetic fields H₁ are stronger in the immediate vicinity of the surface of conductor segment 45 than the fields H₂ in the vicinity of the surface of conductor 46, and thus stronger inductive coupling will occur, and larger currents I₁ will be induced, within the plasma adjacent conductor segment 45 than currents I₂ induced adjacent segment 46. RF power 61 b, 61 a coupled into the plasma adjacent segments 45 will in turn be larger than the RF power 62 a, 62 b coupled adjacent segments 46 (FIGS. 2O and 2F).

Since inductive coupling to the plasma has threshold in RF power below which only capacitive coupling can occur, the low RF power 62 in the region of the large cross-section conductor sector 46 can be such that the ICP mode of coupling is impossible, where the power in the region adjacent the low cross-section sector 45 is still above the ICP threshold level. As a result, coupling of power is concentrated into regions 61 a, 61 b and substantially absent from regions 62 a, 62 b.

Various configurations 43 a-43 e of the segmented conductors 43 are illustrated in FIGS. 3A-3E. Each of these shows a different cross-sectional area configuration, some more effective than others. Generally, three-dimensional distributions such as 43 a and 43 b are more effective, with a dimension extending perpendicular to or away from the window 25, as 43 c, being more effective than parallel to the window as 43 d or 43 e. Instead of segments of differing cross-section, conductor bundles can be made to converge and diverge, as explained more fully below.

FIG. 4 is a cut-away perspective view of the material source 20 of FIG. 1 equipped with a peripheral inductive element for generating ICP in accordance with an embodiment of the invention. The element includes a three-dimensional segmented antenna 40 on the outside of a planar window 25 with a correspondingly segmented deposition baffle or shield 50 protecting the inside of the window 25. Such an element may be that, for example, illustrated in FIG. 2D, producing a plasma power distribution as illustrated in FIG. 2E, which is illustrated in more detail in FIG. 4A.

In FIG. 4A, the antenna 40 a is depicted adjacent dielectric window 25. Baffle 50 a is located on the opposite side of the window 25 from the antenna 40 a. The antenna 40 a is shown as formed of a continuous conductor 43 a having four concentric loops 47 a of six segments each when viewed from the top. A spiral band or a series of rings (not shown) of insulating material, for example of TEFLON, may be interposed between adjacent pairs of the windings 43 a or others of the windings 43 in other embodiments. Each winding 47 a has six small cross-section conductor segments 45 a alternating with six large cross-section conductor segments 46 a, with the segments 45 a,46 a of each winding aligning with similar segments of the adjacent winding 47 a. The small cross-section windings 45 a aligning radially to form radial wedge-shaped high-radiation efficiency portions 41 a of the antenna 40 a and the large cross-sections 45 a aligning radially to form radial wedge-shaped low-radiation efficiency portions 42 a of the antenna 40 a.

The baffle 50 a is shown as a circular metal member having six groups of chevron shaped slots 57 a, which present no line-of-site paths through which particles could move in straight lines through the baffle from the plasma to the window 25. Each group of slots 57 a defines an RF high-transparency portion 51 a of the shield 50 a. The slots 57 a are oriented radially on the baffle 50 a, perpendicular to the high-efficiency conductor segments 45 a of the antenna 40 a, to provide the high-transparency portion 51 a of the baffle 50 a. The areas between the six regions 51 a are of solid metal and define the relatively opaque portions 52 a of the baffle 50 a, which align with the low-efficiency portions 46 a of the conductor 43 a.

To provide circumferential uniformity of the plasma, the fill-factor Φ and cross-section ration Θ are constant from section to section around the circumferences of each of the windings 47, but may differ from winding to winding.

FIG. 4B illustrates a peripheral inductive element similar to that of FIG. 4A, but with an antenna 40 b which has a conductor 43 b with small and large cross-section segments 45 b,46 b formed in parallel straight segments, rather than the curved segments such as segments 45 a,46 a for antenna 40 a. In addition, the antennas 40 may have arches or notches 48 in one surface of the large cross-section segments 46 a, 46 b to further reduce the inductance of these sections of the conductor 43 a, 43 b of the antennas 40. FIGS. 4C, 4D and 4E illustrate alternative antennas 40 c, 40 d and 40 e, respectively, which each have eight radially spaced high and low-efficiency sections 45 and 46 of different configurations. The antennas 40 c and 40 d each have only one winding, while the antenna 40 e has three.

In the embodiments of FIGS. 4-4B, the window 25 can be rotated 30 degrees with respect to the aligned six-segment antennas 40 a-40 b and baffle 50 a to double the mean-time-before-cleaning required for the window 25. Similarly, the window 25 can be rotated 22.5 degrees with respect to the aligned eight-segment antennas 40 c-40 e and corresponding eight-segment baffle (not shown). For large wafers 15 of 300 mm, such windows 25 must be fairly thick in order to withstand the force of atmospheric pressure. Such thick window 25 can be avoided by the use of an array of small window segments 25 a, as illustrated in FIG. 4F. Such window segments 25 a may be made wedge-shaped and positioned to align with the high-efficiency sections of the antenna 45 a and the slotted high-transparency sections 51 a of the shield 50 a. Solid wall segments 54, between the window segments 25 a, may align with the low-efficiency segments 46 of the antenna 40 and the low-transparency segments 52 a of the shield 50 a.

FIG. 5 illustrates a peripheral inductive element of a type suitable for an ICP etch module such as the etch apparatus 30 of FIG. 1A. In such an apparatus, the quartz chamber bell jar-shaped wall 31 may be replaced by a metal wall 31 a having an array of small dielectric windows 25 c therein, each covered by a correspondingly sized baffle 50 c. A helical antenna 40 f encircles the outside of the wall 31 a, with high-efficiency, small conductor sections 45 f aligning with the windows 25 c and low-efficiency sections 45 f aligning with the solid sections of the metal wall 31 a between the window sections 25 c. FIGS. 5A and 5B show alternative forms 40 g, 40 h, respectively, of the antenna 40 f. Referring to FIGS. 5, 5A and 5B, such antennas 40 f, 40 g, 40 h may be formed of a continuous conductor 43 f,43 g,43 h, each having alternating high and low-efficiency sections, the high-efficiency, higher inductance sections 45 f,45 g,45 h being formed of small cross-section conductors and the low-efficiency, lower inductance sections 46 f,46 g,46 h being formed of large cross-section conductors. The apparatus in FIGS. 4A and 5B are shown with a solid bell jar-shaped window 31, as in FIG. 1, in which case, rather than the individual shields 50 c of FIG. 5, a cylindrical shield (not shown) would be provided with high-transparency sections aligned with the high-efficiency sections 45 of the antenna and low-transparency sections aligned with the low-efficiency sections 46 of the antennas 40.

An advantage of the conductors 43 described above that have the large and small cross-section portions is that the cooling of the antenna 50 need not be accomplished by providing hollow tubular conductors with cooling fluid flowing within. The large surface areas of the large cross-section portions of the conductor provide instead substantial thermal conductivity to provide ample cooling of the conductor by heat exchange with the surrounding medium.

FIG. 6 illustrates a cut-away portion of an etch module 30 a similar to that of FIGS. 5-5B having a particularly cost-effective peripheral inductive element that can be manufactured using simple ICP source construction techniques. In FIG. 6, the dielectric wall 31 of the etch module 30 a is surrounded by a modified helical antenna 40 i that utilizes multiple windings of a conductor 43 i formed of small size tubing throughout its length. The conductor 43 i is configured to provide the advantages of the varying cross-section segmented antenna conductors 43 described above. A deposition shield 50 d is provided on the inside of the bell jar-shaped dielectric wall 31. The shield 50 d has high and low-transparency sections 55 d,56 d that respectively correspond to and radially align with high-efficiency sections 45 i of the antenna 40 i, in which the windings lie close together, and low-efficiency sections 46 i of the antenna 40 i, in which the windings are spread apart. The alternating closely-shaped or bundled conductors and spaced-apart or diverging conductor sections, 45 i and 46 i, respectively, of antenna 40 i, have high and low-inductance and radiation efficiency, because the spreading of the conductors results in magnetic fields that oppose each other close to and between the individual conductor windings in the diverging sections 46 i, while the closeness of the conductors results in magnetic fields that enforce each other by encircling the entire bundled conductor sections 45 i.

In FIG. 6, the inductive element 43 i is created by the tubular conductor 43 i that is azimuthally divided into multiple sections, for example, eight sections, with the high and low-efficiency sections 45 i, 46 i each spanning 22.5 degrees. The pitch between individual loops is small in the high-efficiency, bundled-conductor sections 45 i to generate locally stronger RF magnetic fields in the plasma. The pitch between individual loops is large in the low-efficiency, diverging-conductor sections 46 i to generate reduced RF magnetic fields when passing through the dielectric wall.

The baffle 50 d in the embodiment of FIG. 6 is generally cylindrical and surrounds the inside sidewall of the bell jar-shaped dielectric 31 directly opposite the antenna 40 i, and generally protects the window from deposits around its cylindrical peripheral sidewall. The top portion of the dielectric 31 is not protected by the baffle 50 d, but because the antenna does not rely on coupling through this portion, deposits on this portion do not interfere with the efficiency of the plasma generation. The high-transparency sections 55 d, which align with the high-efficiency sections 45 i of the antenna 40 i, block all but minimal deposition on the dielectric 31, where the opaque sections 56 d almost totally prevent deposits on the adjacent sections of the dielectric. Nonetheless, deposits of metal on the dielectric 31 adjacent the high-transparency sections 55 d eventually begin to reduce RF coupling through the dielectric 50 d at these portions. When this condition is reached, the antenna 40 i can be rotated by 22.5 degrees to move the areas of accumulated deposits on the window 31 to double the mean-time-before-cleaning (MTBC) of the window.

The antenna 50 d also has one of the windings, namely winding 47 a, in the divergent sections 46 i of the antenna 40 i, extending partially around to the top side of the dielectric window 31, beyond the extent of the baffle 50 d. Such extended windings 47 a have a small capacitive coupling with the plasma and, as a result, are effective in coupling energy to the plasma during plasma ignition.

FIGS. 6A, 6D and 6G illustrate antennas 40 j, 40 k, and 40 l, respectively, that are variations of the antenna 40 i of FIG. 6, where the windings are configured in six alternating sections spanning 30 degrees each. The antenna 40 j may be used, in place of the antennas 40 f, 40 g and 40 h, with the shields similar to those of FIGS. 5, 5A and 5B or with the shield 50 e of FIG. 6B, producing the energy distribution 60 c of FIG. 6C. Peak power density is approximately up to 0.48 Wcm⁻² in regions 61 c of FIG. 6F at 10 amp current through inductive element 40 j, with little deposited power in regions 62 c. Total deposited power into plasma is about 316 watts at these conditions.

Antennas 40 k and 40 l are configured in a honeycomb structure and may be used with the appropriate shields, including shields 50 f and 50 g, respectively, of FIGS. 6E and 6H, producing the energy distributions 60 d and 60 e of FIGS. 6F and 6G. The shield 50 e has a single row of full-height alternating high-transparency and opaque sections 55 e and 56 e, respectively, to align with the high and low-efficiency sections 45 j and 46 j of the antenna 40 j. Shield 50 f has two staggered rows of alternating high-transparency and opaque sections 55 f and 56 f, respectively, to align with the high and low-efficiency sections 45 k and 46 k of the antenna 40 k, while shield 50 g has three staggered rows of alternating transparency and opaque sections 55 g and 56 g, respectively, to align with the high and low-efficiency sections 45 l and 46 l of the antenna 40 l.

For the honeycomb structure of the conductors within the antennas 40 k, peak power density is approximately 0.19 Wcm⁻² in the regions 61 d of FIG. 6F with little power deposited in the regions 62 d. Total deposited power into plasma is approximately 220 watts. Inductance of the antenna 40 k is less than for antenna 40 j, e.g. 8.34 mH for antenna 40 l versus 10.73 mH for antenna 40 j. For antenna 40 l, peak power density is 0.30 Wcm⁻² in regions 61 e of FIG. 6J with little deposited power in regions 62 e. Total power is 235 watts at 10 amps, 450 kHz, with inductance at 8.59 mH.

The deposition shields 50 e, 50 f and 50 g of FIGS. 6B, 6E and 6H have the high-transparency portions 55 e, 55 f and 55 g adjacent the areas of reduced pitch of the respective antennas 40 j, 40 k and 40 l.

FIGS. 7A and 7B illustrate cost effective embodiments 40 m and 40 n of antennas suitable for an iPVD application as illustrated in FIG. 4. The antennas 40 m and 40 n each have high-efficiency sections 45 m, 45 n and low-efficiency sections 46 m, 46 n, each having constant cross-section tubular conductors with modulated pitch structure. Deposition baffles 50 f and 50 g are designed for use with antennas 45 m and 45 n, respectively, and have sections of high-transparency, 55 f, 55 g and opacity 56 f, 56 g, configured and aligned with the antenna sections according to the principles described above.

Antenna 40 o of FIG. 7C is a preferred three-dimensional embodiment of an antenna that can be efficiently used with the baffle 50 f (FIG. 7A). It includes six 30 degree sections 45 o of closely-spaced conductors alternating with six 30 degree sections 46 o of diverging conductors that extend away from the plane of the shield 50 f. The concentrated high-efficiency sections 45 o of the antenna 40 o align with the high-transparency sections 55 f of the shield 50 f while the divergent low efficiency sections of the antenna 40 o align with the opaque sections 56 f of the shield 50 f.

Advantages and benefits of the disclosed configurations include doubling of the lifetime of dielectric bell jar of FIG. 6 or window 25 of FIG. 4, by rotation of the dielectric, taking advantage of only a portion of the window being directly exposed to plasma and contamination. With these and other embodiments described above, ohmic losses into deposition shield 500 are less than with the prior art. Reliable plasma ignition is provided, particularly with the configuration of FIG. 6, by extending the winding 47 a of the antenna 40 i that extends beyond the shield 50 d, where it can capacitively couple energy through the window to ignite the plasma. Partially opaque deposition shields can be used without losing power due to reduced inductive coupling. RF power deposition into the plasma is increased in pre-selected locations, which can be tailored by inductive element design by varying antenna pitch value of the antenna sections and the ratio between “low” and “high” transmission areas of the deposition shield. Intense RF magnetic fields are generated locally, increasing deposited power into the plasma even through slots in the deposition shield that are relatively short. Little RF power is lost in the opaque shield areas.

The invention has been described in the context of exemplary embodiments. Those skilled in the art will appreciate that additions, deletions and modifications to the features described herein may be made without departing from the principles of the present invention. Accordingly, the following is claimed: 

1-19. (canceled)
 20. A low-inductance RF antenna for inductively coupling energy to a high-density plasma in a vacuum chamber for the plasma processing of a semiconductor wafer, the antenna comprising: a segmented configuration formed of an alternating plurality of high and low-efficiency antenna segments, the high-efficiency segments including concentrated current-carrying segments producing relatively high magnetic fields externally adjacent and surrounding the high-efficiency segments and the low-efficiency segments including distributed current-carrying segments producing relatively low magnetic fields externally adjacent and surrounding the low-efficiency segments.
 21. The antenna of claim 20 wherein: the high-efficiency segments are formed of relatively small cross-section conductor sections and the low-efficiency segments are formed of relatively large cross-section conductor sections.
 22. The antenna of claim 20 further comprising: a plurality of conductor windings; and the high-efficiency segments of the antenna being formed of closely spaced conductor sections of different windings and the low-efficiency segments are formed of conductor sections of different windings that are more widely spaced than the closely spaced conductor sections.
 23. The antenna of claim 20 wherein the high-efficiency antenna segments and the low-efficiency antenna segments are alternately arranged in a ring around a central axis.
 24. The antenna of claim 20 further comprising: a conductor having at least one winding around a central axis, the conductor having an alternating series of small cross-section portions and large cross-section portions angularly spaced around the central axis; each of the high-efficiency segments being formed of one or more of the small cross-section portions of the conductor and each of the low-efficiency segments being formed of one or more of the large cross-section portions of the conductor; whereby the conductor has a configuration that provides the antenna with the segmented configuration of alternating high and low-efficiency segments arranged in a ring about the central axis.
 25. The antenna of claim 20 wherein: the high-efficiency segments provide concentrated antenna current paths, and the low-efficiency segments provide distributed antenna current paths, for currents in the conductor, which provide a ring of alternating high and low strength magnetic fields external to the conductor, which energize a ring-shaped plasma having alternating high and low plasma density regions.
 26. The antenna of claim 20 wherein: the antenna has a segmented cylindrical configuration; the conductor includes at least one winding wound around a central axis.
 27. The antenna of claim 20 wherein: the antenna has a segmented planar configuration; the conductor includes at least one winding lying in a plane and wound around a central axis that is perpendicular to the plane.
 28. The antenna of claim 20 further comprising: a conductor having a plurality of windings surrounding an axis; each of the high-efficiency segments of the antenna being formed of closely spaced portions from each of a plurality of the windings of the conductor, and each of the low-efficiency segments being formed of relatively widely spaced portions from each of a plurality of the windings of the conductor.
 29. The antenna of claim 28 wherein: the high-efficiency segments provide concentrated antenna current paths, and the low-efficiency segments provide distributed antenna current paths, for currents in the conductor, which provide a ring of alternating high and low strength magnetic fields external to the conductor, which energize a ring-shaped plasma having alternating high and low plasma density regions.
 30. The antenna of claim 28 wherein: the antenna has a segmented cylindrical configuration.
 31. The antenna of claim 28 wherein: the windings lie in a plane.
 32. An antenna for inductively coupling energy into a high-density plasma in a vacuum chamber for processing a semiconductor wafer therewith, the antenna comprising: at least one conductor having at least one winding around a axis, the conductor being configured to provide the antenna with a segmented configuration of alternating high and low-efficiency segments arranged in a ring about the axis; the high-efficiency segments including concentrated-current-carrying portions producing, when currents pass therethrough, relatively high magnetic fields external to and surrounding the sections of the at least one conductor within the high-efficiency segments; and the low-efficiency segments including distributed-current-carrying portions, producing, when currents pass therethrough, magnetic fields external to and surrounding the high-efficiency segments that are relatively low compared to those produced by the high efficiency segments, the distributed-current-carrying portions allowing more of the magnetic fields to pass therethrough and to cancel than pass through the concentrated-current-carrying portions, and thereby produce lower magnetic fields external thereto; whereby, when RF current is applied to the at least one conductor and inductively coupled therefrom into a plasma within a vacuum chamber of a processing apparatus, more power couples from the high-efficiency segments to the plasma adjacent thereto than couples from the low-efficiency segments to the plasma adjacent thereto, thereby producing an alternating ring-shaped array of high and low density plasma regions within the chamber.
 33. The antenna of claim 32 wherein: the high-efficiency segments of the antenna are formed of small cross-section sections of the at least one conductor and the low-efficiency segments of the antenna are formed of relatively large cross-section sections of the at least one conductor.
 34. The antenna of claim 32 wherein: the at least one conductor has a plurality of windings around the axis; the high-efficiency segments of the antenna are formed of a plurality of closely spaced conductor sections of different windings of the plurality of windings, and the low-efficiency segments of the antenna are formed of a plurality of conductor sections of different windings of the plurality of windings that are substantially more widely spaced than the closely spaced conductor sections.
 35. An antenna for inductively coupling energy into a high-density plasma in a vacuum chamber for processing a semiconductor wafer therewith, the antenna comprising: means for producing an alternating array of high and low density plasma regions within the chamber, including alternating high and low-efficiency antenna segments; the high-efficiency antenna segments including means for producing relatively high magnetic fields external thereto; and the low-efficiency antenna segments including means for producing relatively low magnetic fields external thereto.
 36. The antenna of claim 35 wherein: the high-efficiency segments are high-current-density segments; and the low-efficiency segments are low-current-density segments.
 37. The antenna of claim 35 wherein: the high-efficiency segments include at least one small-cross-section conductor section and the low-efficiency segments include at least one large-cross-section conductor section.
 38. The antenna of claim 35 wherein: the high-efficiency segments of the antenna include a plurality of closely-spaced conductor sections of different conductor windings and the low-efficiency segments of the antenna include a plurality of conductor sections that are more widely spaced than the closely-spaced conductor sections.
 39. The antenna of claim 35 further comprising: one or more generally circular windings arranged in a plane.
 40. The antenna of claim 35 further comprising: a plurality of generally circular windings arranged in a cylinder.
 41. The antenna of claim 35 wherein: the antenna includes a conductor having at least one winding around a central axis and presenting a plasma side facing into a processing space in the chamber; the plurality of high efficiency segments are spaced at equal intervals around the axis and configured to concentrate current and produce relatively high magnetic fields adjacent to the conductor on the plasma side thereof, and the plurality of low efficiency segments are spaced at equal intervals around the axis between adjacent high efficiency segments and configured to more widely distribute current therein and produce relatively low magnetic fields adjacent to the conductor on the plasma side thereof; the high and low efficiency segments being arranged in a ring so as to couple power from the plasma side thereof into the processing space within the chamber to energize a plasma in the processing space in an annular alternating high and low power density distribution. 